FIELD: military equipment.
SUBSTANCE: invention relates to military equipment and can be used in creation of noise-proof proximity sensors of various ammunition targets, including missiles with homing heads on target. Method of identifying a target using a radio fuse of a missile with a homing head consists in that, using a radio fuse generator after time intervals Ti, short radio frequencies of duration τ (τ<<Ti) are generated in the radiating antenna of the radio fuse. Receiving antenna of radio fuse is used to receive radio pulses continuously in gating interval Tst. At that, using the radar station of the missile self-guidance head in real time for each time interval Ti the speed of approach of the missile is determined with the aim of VsG. With channel information processing of radio fuse for each time interval Ti is calculated target distance Si, using the relation Si=cti/2, where c – velocity of light, ti – time from the beginning of the radiation generator before the pulse in the information processing channel. For each two consecutive radiation periods, the rate of approach of the missile is calculated for the purpose of Vc, using the ratio Vc=(Si-Si+1)/Ti, where Si+1 is the distance to the target in the next time interval ti+1, for each time interval Ti. Comparing the calculated values of VsG and Vc. From the ratio of the velocities identified taken during Tst strobe signals are reflected from the targets. Based on the comparison results, a decision is made to actuate the detonating fuse according to a predetermined algorithm.
EFFECT: invention increases noise immunity of proximity sensors of missile target using missile self-guided homing heads against artificial interference.
1 cl, 1 dwg
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Authors
Dates
2020-06-04—Published
2019-10-23—Filed